Bayraktar TB2 / Mohajer-6 · Comparison
Choose 2–4 types. A shared unit does not make different missions, variants or source methods equivalent. Only source-bound observations are compared.
One scale. Different machines.
Bayraktar TB2 · TB2 · Baykar · Source notebook
Mohajer-6 · Mohajer-6 · ODIN family entry · Source notebook
Human height is an illustrative 1.8 m; bus length an illustrative 12 m. Car length uses the cited MINI specification. Vehicle heights and drone side contours are schematic. Top views preserve published length and span; an absent dimension is never guessed.
One car length here is 3.821 m: MINI Cooper 3 door, March 2020 specification.
Solid segments show published intervals; dashed segments have an open endpoint. They are source bounds, not statistical confidence intervals. Each row has its own linear scale; longer is not a quality score.
| The numbers, with their sources | Bayraktar TB2 | Mohajer-6 |
|---|---|---|
| Published flight range | Unknown in reviewed sources | Unknown in reviewed sources |
| Reported speed | Unknown in reviewed sources | Unknown in reviewed sources |
| Published speed · knots | 90–110 kt[1] | Unknown in reviewed sources |
| Take-off mass | 700 kg[1] | Unknown in reviewed sources |
| Payload | 150 kg[1] | Unknown in reviewed sources |
| Warhead mass | Unknown in reviewed sources | Unknown in reviewed sources |
| Body length | 6.4 m[1] | 5.67 m[2] |
| Wingspan | 12 m[1] | 10 m[2] |
| Width · propellers excluded | Unknown in reviewed sources | Unknown in reviewed sources |
| Hull beam | Unknown in reviewed sources | Unknown in reviewed sources |
| Flight duration | Unknown in reviewed sources | Unknown in reviewed sources |
| Endurance | ≥ 18 h[1] | Unknown in reviewed sources |
| Communication distance | Unknown in reviewed sources | Unknown in reviewed sources |
| Published sailing range · nautical miles | Unknown in reviewed sources | Unknown in reviewed sources |
| Published sailing range | Unknown in reviewed sources | Unknown in reviewed sources |
Intervals preserve the published bounds; they are not statistical confidence intervals. A blank lower or upper bound stays open. Values belong to the named configuration, not every aircraft.